GATE AE · 2018 · AE
Question 43: Airplane Performance
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Question 43
AENAT2 marksNeeds review
A pitot probe on an aircraft in a steady, level flight records a pressure of 55,000 N/m
. The static pressure and density are 45,280 N/m
and 0.6 kg/m
, respectively. The wing area and the lift coefficient are 16 m
and 2, respectively. The wing load (in N/m
) on this aircraft is ________ (accurate to one decimal place).Log in to check the answer
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2018AE
GATE AE 2018 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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